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Type: Fighter Origin: Curtiss Aeroplane and Motor Company Crew: One Model: P-36, Model 75, Hawk 75 Contract Price: $23,000 |
First Flight: May 1935 Service Delivery: 1938 Retired: 1954, Argentina Aircraft Produced: 845 |
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Powerplants: Model: Pratt & Whitney R-1830-13 Twin Wasp Type: air-cooled radial engine Number: One Horsepower: 1,050 hp Dimensions: Wing span: 37 ft. 4 in. (11.3m) Length: 28 ft. 6 in. (8.7m) Height: 8 ft. 5 in. (2.8m) Wing Surface Area: 235.6 ft² (21.9 m²)
Weights: |
Performance: Maximum Speed: 322 mph (518 km/h) Cruising Speed: 260 mph (420 km/h) Rate of climb: 2,500 ft/min (13 m/s) Service Ceiling: 32,340 ft (9,860 m) Wing loading: 25 lb/ft² (122 kg/m²) Power/mass: 0.18 hp/lb (0.29 kW/kg) Range: 650 mi (1,046 km) Armament: Two .30 machine guns Or Two .50 machine guns |
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The Curtiss P-36 Hawk, also known as Curtiss Hawk Model 75, was a U.S.-built fighter aircraft of the 1930s. A contemporary of the Hawker Hurricane and Messerschmitt Bf 109, it was one of the first fighters of the new generation – sleek monoplanes with extensive use of metal in construction and powerful piston engines. Obsolete at the onset of World War II and best known as the predecessor of the Curtiss P-40, the P-36 saw only limited combat with the United States Army Air Forces but was extensively used by the French Air Force and also by British Commonwealth and Chinese air units. Several dozen also fought in the Finnish Air Force against the Soviet Red Air Force. With around 1,000 aircraft built, the P-36 was a major commercial success for Curtiss. |
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Design and development The Curtiss Model 75 was a private venture by the company, designed by former Northrop engineer Donovan Berlin. The first prototype constructed in 1934 featured all-metal construction with fabric-covered control surfaces, a Wright XR-1670-5 radial engine developing 900 hp (671 kW), and typical U.S. Army Air Corps armament of one 0.30-cal. and one 0.50-cal. machine guns firing through the propeller arc. Also typical of the time was the total absence of armor or self-sealing fuel tanks. The distinctive landing gear which rotated 90 degrees to fold the main wheels flat into the thin trailing portion of the wing was actually a Boeing-patented design for which Curtiss had to pay royalties.
![]() P-36 Hawk. Source: Unknown
![]() P-36 Hawk. Source: Unknown
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Variants: Model 75A - company-owned demonstrator aircraft flown with several engine fits Model 75B - prototype with Wright R-1820 engine Model 75D - first prototype, Wright R-1670 engine Model 75H - internal company designation for a simplified export version with fixed landing gear, two slightly differing aircraft built, first sold to China, second to Argentina Model 75J - company-owned 75A temporarily fitted with an external supercharger Model 75K - Unbuilt version, it was going to be powered by a Pratt & Whitney R-02180 Twin Hornet engine. Model 75P - production P-36A (serial 38-010) fitted with Allison V-1710 liquid-cooled engine, prototype for Curtiss P-40 Model 75R - company-owned 75A temporarily fitted with R-1830-SC2-G engine with turbosupercharger, attained 330 mph (530 km/h) but proved complex and unreliable
Curtiss P-36's involved in pre-WWII manuevers. Source: UnknownP-36A (Model 75L) - USAAC version, P-26A-3 mounted four 0.30 in machine guns in the wings in addition to fuselage armament P-36B - production P-36A fitted with an R-1830-25 engine producing 1,100 hp (820 kW), reached 313 mph (504 km/h), returned to original P-36A configuration P-36C - an additional 0.30 in machine gun installed in each wing with external ammunition boxes under the wings, R-1830-17 engine with 1,200 hp (895 kW), last 30 production aircraft were completed as P-36Cs XP-36D - production P-36A modified with 2 x 0.50 in machine guns in the nose and 4x 0.30 in machine guns in the wings XP-36E - production P-36A armed with 4 x 0.30 in machine guns in the wings, retained standard fuselage guns XP-36F - production P-36A fitted with 2 x 23 mm Madsen cannons under the wings, reverted to P-36A because guns imposed an unacceptable performance penalty with top speed of only 265 mph (427 km/h) P-36G - Hawk 75A-8 used by Norway for training in Canada, later to Peru. Wright R-1820-G205A with 1,200 hp (895 kW). Hawk 75A-1 - 1st production batch for France, 4 x 7.5 mm machine guns, R-1830-SC-G engine with 900 hp (671 kW), 100 built Hawk 75A-2 - 2nd production batch for France, either R-1830-SC-G engine or 1,050 hp (783 kW) R-1830-SC3-G engine, 6 x 7.5 mm machine guns, 100 built Hawk 75A-3 - 3rd production batch for France, similar with Hawk 75A-2, 135 built Hawk 75A-4 - Last production batch for France, Hawk 75A-2 with Wright R-1820-G205A Cyclone engine with 1,200 hp (895 kW). 285 built, 81 delivered to France, others to Great Britain as Mohawk IV Hawk 75A-5 - built under license in China (production was later moved to India), absorbed into RAF as Mohawk IV Hawk 75A-6 - version for Norway, captured aircraft sent to Finland Hawk 75A-7 - version for Netherlands East Indies: 1,200 hp Cyclone, 4 x 7.7 mm (two in nose, one in each wing) and 2 x 100 lb bombs. Hawk 75A-8 - Export version for Norway. Later redesignated P-36G. Hawk 75A-9 - 10 aircraft delivered to Persia, captured still in crates and used by RAF in India as Mohawk IVs Hawk 75M - simplified version with fixed landing gear and Wright R-1820 Cyclone engine for China, built by both Curtiss and Central Aircraft Manufacturing Company in China Hawk 75N - simplified version for Siam (Thailand) Hawk 75O - simplified version for Argentine, 29 built by Curtiss with additional 200 built under license locally by Fabrica Militar de Aviones Hawk 75Q - two additional simplified demonstrators for China XP-37 - Allison V-1710 liquid-cooled engine, cockpit moved to the rear of the fuselage YP-37 - service test version of XP-37, 13 built XP-42 (Model 75S) - testbed for streamlining cowlings around air-cooled engines |